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Experimental Heat Transfer and Discharge Coefficients for Single Confined Jet Impingement Normal to a Surface at Close Distances

机译:法向近距离垂直于表面的单约束射流冲击的实验传热和排放系数

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Heat transfer and flow discharge coefficients for confined jet impingement are being investigated for a single round jet impinging normal to a target surface less than one hole diameter from the jet origin. A search of open literature resulted in the availability of no discharge coefficient information, and limited heat transfer information, especially for the configuration of a confined jet in close surface impingement. The experiment has been conducted for a developing jet and utilizes liquid crystal thermography for heat transfer measurements. Nusselt numbers were obtained for jet Reynolds numbers between 15000 and 30000 with a gap to hole diameter ratio of 0.3 to 3. Discharge coefficient data were obtained for jet Reynolds numbers between 11000 and 59000, with a gap to hole diameter ratio of 0.2 to infinity. The heat transfer data obtained shows a secondary Nusselt number peak and similar trends to those seen in other close surface impingement studies. The data also show a crossover of Nusselt number at increasing radial distance from the jet stagnation point with increasing gap size which could be indicative of ambient air entrainment. The discharge coefficient data obtained show a decrease in discharge coefficient for a decrease in gap size. At constant pressure ratio con-ditions a large decrease in discharge coefficient is observed between pressure ratios of 1.05 and 1.11. The results of this study are applicable to many industrial applications. However, a discussion of close surface impingements applicability to gas turbines has been included, as well as a comparison of the experimental and numerical results.
机译:对于与目标表面垂直的单个圆形射流,从射流起点开始,其传热和流量排放系数正在研究,该射流法向垂直于目标表面,且射流直径小于一个射孔直径。公开文献的搜索导致没有排放系数信息,并且传热信息有限,特别是对于密闭表面撞击中的受限射流构型。该实验是针对显影喷嘴进行的,并利用液晶热像仪进行传热测量。间隙与孔径之比为0.3到3时,雷诺数为15000到30000时获得了Nusselt数。间隙与孔径之比为0.2到无穷大时,雷诺数为11000到59000之间时,得到了放电系数数据。获得的传热数据显示了次级Nusselt峰,并且与其他近表面冲击研究中所看到的趋势相似。数据还显示,随着距喷嘴停滞点径向距离的增加,间隙尺寸增大,努塞尔数越过,这可能表明环境空气夹带。所获得的放电系数数据表明,随着间隙尺寸的减小,放电系数减小。在恒压比下, 在压力比为1.05和1.11之间观察到排放系数大大降低。这项研究的结果适用于许多工业应用。但是,已经讨论了对燃气轮机的近表面撞击适用性,并进行了实验和数值结果的比较。

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